# Service difficulty reports: N793AX

A list on [N793AX](https://openairdocs.org/aircraft/N793AX.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 3 · 101 reports

- [SDR ABXA20160314042](https://openairdocs.org/sdr/ABXA20160314042.md): Strap · corroded · Mar 14, 2016 · N793AX · Boeing 767281 · Fuselage Main, Frame
  > STATION 955 LT FAILSAFE HAS HFEC DEFECT INDICATION AFT SIDE OF FAILSAFE TRIM OUT. R & R FAILSAFE STRAP & INSTALLED IAW DOCUMENT 470080RD11. SDR INFO CRACKED LENGTH 3.75", PN 145T2524-19, PART NAME FAILSAFE STRAP, SN NSN, FS & BS FROM 955, STRINGER & WS FROM
- [SDR ABXA20160314038](https://openairdocs.org/sdr/ABXA20160314038.md): Failsafe · cracked · Mar 14, 2016 · N793AX · Boeing 767281 · Fuselage Main, Frame
  > LEFT FAIL SAFE LOWER HOLE CRACKED. R & R FAILSAFE STRAP & INSTALLED IAW DOCUMENT 470080RD11. CRACKED LENGTH 3.75", PN 145T2524-19, PART NAME, FAILSAFE STRAP, SN NSN, FS & BS FROM 955, STRINGER & WS FROM 52DL. ACFT WAS GNDED.
- [SDR ABXA20160314036](https://openairdocs.org/sdr/ABXA20160314036.md): Tee Fitting · corroded · Mar 14, 2016 · N793AX · Boeing 767281 · Fuselage Miscellaneous Structure
  > PRESSURE DECK T FITTING IS CORRODED AT THE LOWER BOLT HOLE, STATION 955 LT SIDE. R & R T FITTING, INSTALLED ON DOCUMENT 470080RD11 STEP 44. REPLACEMENT PART MARKED DRILLED IAW SRM 51-40-05. CORRODED LEVEL 2, PN 100T1440U3, PART NAME, T FITTING, SN NSN, FS &
- [SDR ABXA20160309044](https://openairdocs.org/sdr/ABXA20160309044.md): Fitting · corroded · Mar 9, 2016 · N793AX · Boeing 767281 · Fuselage Main, Attach Fittings
  > LEFT WW FWD SPAR KICK FITTING HAS 2 EACH FASTENER HOLES CORRODED. REPAIRED CORRODED HOLES IAW REA B657-61967 MR. SDR INFO CORRODED LEVEL 2, PN 112T1219-7, PART NAME KICK LOAD FITTING, SN NSN, FS & BS FROM 955, STRINGER & WS FROM CTR FUSE I CTR WING. ACFT WAS
- [SDR ABXA20160308045](https://openairdocs.org/sdr/ABXA20160308045.md): Fitting · damaged · Mar 8, 2016 · N793AX · Boeing 767281 · Fuselage Main, Attach Fittings
  > LEFT SIDE FRAME FITTING HAS AN EXISTING OVERSIZED HOLE WITH A BUSHING COMMON TO THE KICK FITTING. SIDE FRAME FITTING OVERSIZED HOLES WERE REPAIRED IAW REA B653-61969 MR. SDR INFO CORRODED LEVEL 2, PN 145T2523-5, PART NAME SIDE FRAME FITTING, SN NSN, FS & BS
- [SDR ABXA20160308040](https://openairdocs.org/sdr/ABXA20160308040.md): Skin · corroded · Mar 8, 2016 · N793AX · Boeing 767281 · Fuselage Main, Plate/Skin
  > LEFT WW STATION 955, SKIN COMMON TO FAILSAFE TRIM OUT AREA CORRODED. REMOVED CORROSION ON SKIN IAW EA 53500013-004 & REPAIRED AREA IAW REA B653-61969-MR. SDR INFO CORRODED LEVEL 2, PN 145T3320-11, PART NAME, FUSELAGE SKIN, SN NSN, FS & BS FROM 955, STRINGER
- [SDR ABXA20160302039](https://openairdocs.org/sdr/ABXA20160302039.md): Failsafe · cracked · Mar 2, 2016 · N793AX · Boeing 767281 · Wing Main, Frame Structure
  > RIGHT WING FAILSAFE BOTTOM HOLE CRACKED. ACCOMPLISHED TRIM OUT & REWORK OF FAILSAFE STRAP IAW DOCUMENT 470080RD04 STEPS 1 - 9. SEE 470080RD04 FOR ALL OTHER REWORK & ASSEMBLY STEPS. CRACKED LENGTH.500, PN 145T2524-20, PART NAME, FAILSAFE STRAP, SN NSN, FS &
- [SDR ABXA20160301037](https://openairdocs.org/sdr/ABXA20160301037.md): Tee Fitting · corroded · Mar 1, 2016 · N793AX · Boeing 767281 · Fuselage Miscellaneous Structure
  > PRESSURE DECK T FITTING IS CORRODED AT THE LOWER BOLT HOLE, STATION 955 RT SIDE. R & R T ANGLE FITTING IAW EA 53500014-003 STEP 15 - 16, & SRM 51-40-02. CORRODED LEVEL 2, PN 11DT1440U4, PART NAME, T FITTING, SN NSN, FS & BS FROM 955, STRINGER & WS FROM 52DR
- [SDR ABXA20160227043](https://openairdocs.org/sdr/ABXA20160227043.md): Skin · corroded · Feb 27, 2016 · N793AX · Boeing 767281 · Fuselage Main, Plate/Skin
  > STATION 955 IN THE AREA OF FAILSAFE TRIM OUT ON THE RT FUSELAGE SKIN, LOWER HOLE, THE SPOTFACE HAS EXCEEDED THE.324 MINIMUM ALLOWABLE THICKNESS. SPOTFACE AREA REPAIRED IAW REA 6653-61962 MR. SDR INFO CORRODED LEVEL 2, PN 145T3420-11, PART NAME FUSELAGE SKIN
- [SDR ABXA20160226041](https://openairdocs.org/sdr/ABXA20160226041.md): Skin · corroded · Feb 26, 2016 · N793AX · Boeing 767281 · Fuselage Main, Plate/Skin
  > RIGHT WW STATION 955, SKIN COMMON TO FAILSAFE TRIM OUT AREA CORRODED. REMOVED CORROSION IAW SRM 51-10-02, DOCUMENT 47008 ORD STEP 3 & EA 53500014-004. SDR INFO CORRODED LEVEL 2, PN 145T3420-11, PART NAME FUSELAGE SKIN, SN NSN, FS & BS FROM 955, STRINGER & WS
- [SDR ABXA20150730089](https://openairdocs.org/sdr/ABXA20150730089.md): Angle · cracked · Jul 30, 2015 · N793AX · Boeing 767281 · Wing Miscellaneous Structure
  > FRONT SPAR TO LE ANGLE, ABOVE & AFT OF SLAT PDU CRACKED AT LOWER END. REMOVED & INSTALLED SERVICEABLE LOWER FRONT SPAR TO LE ANGLE ABOVE & AFT OF SLAT PDU IAW SRM 51-40-02 PARA 7, NO LEAKS NOTED. CRACKED 2 INCHES, PN 14T1342U105, PART NAME ANGLE, WING LE, SN
- [SDR ABXA20150729110](https://openairdocs.org/sdr/ABXA20150729110.md): Support Beam · corroded · Jul 29, 2015 · N793AX · Boeing 767281 · Wing Miscellaneous Structure
  > RIGHT WING UPPER TE PANEL SUPPORT BEAM AT WS 349 - 325 HAS A HOLE CORRODED THRU AT A NUTPLATE. R & R RT WING TE PANEL SUPPORT BEAM AT WS 349 - 325 IAW SRM 51-40-02 PARA 7 D. CORRODED L2, PN 113T1632-70AX, SN N/A, PART NAME SUPPORT, STR & WS LOCATION ON ACFT
- [SDR ABXA20150729108](https://openairdocs.org/sdr/ABXA20150729108.md): Structure · corroded · Jul 29, 2015 · N793AX · Boeing 767281 · Wing Miscellaneous Structure
  > SMALL AREA OF CORROSION ON UPPER TE PANEL ATTACH CHORD ON INBD END AS SEEN THRU PANEL 552AB OPENING. R & R ATTACH CHORD SECTION IAW SRM 57-51-02. CORRODED L2, PN 113T1406-5, SN N/A, PART NAME CHORD, WS LOCATION ON ACFT WS 280 - 298, ACFT WAS GNDED.
- [SDR ABXA20150728109](https://openairdocs.org/sdr/ABXA20150728109.md): Support Beam · corroded · Jul 28, 2015 · N793AX · Boeing 767281 · Wing Miscellaneous Structure
  > RIGHT WING, TE UPPER CHORD OF THE INBD SPOILER SUPPORT BEAM IS CORRODED AT WS 365 - 370. INSTALLED NEW CHORD PART 113T1406-6 IAW REA B657-61649MR & SRM 51-40-02. CORRODED L2, PN 113T1406-6, SN N/A, PART NAME CHORD, FS & BS LOCATION ON ACFT RT WING TO TE, STR
- [SDR ABXA20150728098](https://openairdocs.org/sdr/ABXA20150728098.md): Support · corroded · Jul 28, 2015 · N793AX · Boeing 767281 · Wing Miscellaneous Structure
  > REAR SPAR TO TE UPPER PANEL, ATTACH CHORD AT WS 360, CORRODED AROUND NUTPLATES AT AFT END. R & R REAR SPAR TO TE UPPER PANEL ATTACH CHORD AT WS 360 IAW DWG 113T1626 & REA B657-61627. CORRODED L2, PN 113T1626-44, SN NONE, PART NAME CHORD, UPPER SUPPORT, STRIN
- [SDR ABXA20150724119](https://openairdocs.org/sdr/ABXA20150724119.md): Longeron · cracked · Jul 24, 2015 · N793AX · Boeing 767281 · Fuselage Main, Longeron/Stringer
  > UPPER LONGERON WEB HAS A 2 INCH CRACK AT FS 1800 - 1806. INSTALLED NEW WEB & BRACKETS IAW SRM 51-40-02. SDR INFO, CRACK 2 INCHES, PART NUMBER 148T9120-11, PART NAME LONGERON WEB, SN NA, EXACT FS & BS LOCATION ON ACFT 1800 TO 1806. ACFT WAS GNDED.
- [SDR ABXA20150724096](https://openairdocs.org/sdr/ABXA20150724096.md): Structure · corroded · Jul 24, 2015 · N793AX · Boeing 767281 · Wing Miscellaneous Structure
  > WING TE LOWER PANEL ATTACH CHORD, 32 INCHES FROM REAR SPAR & 25 INCHES FROM OTBD SIDE OF INBD FLAP, OTBD HINGE PARALLEL TO REAR SPAR SPLIT ON EDGE. R & R PANEL ATTACH CHORD FOR PANEL 652JB IAW SRM 51-40-02 & REA B657-61646-MR. CORRODED LEVEL 2, PN 113T1407-2
- [SDR ABXA20150723107](https://openairdocs.org/sdr/ABXA20150723107.md): Channel · corroded · Jul 23, 2015 · N793AX · Boeing 767281 · Fuselage Miscellaneous Structure
  > ALL THREE HYD LINE CLAMP BLOCKS CORRODED AT BRACKET ATTACH POINT AS SEEN THRU PANEL 552AB OPENING. REMOVED, FABRICATED & REPLACED THREE HYD LINE CLAMP BOCKS INSIDE PANEL 552AB OPENING IAW DWG 113T1101 & SRM 51-40-02. CORRODED L2, PN 65B80254-304, SN N/A, PAR
- [SDR ABXA20150722101](https://openairdocs.org/sdr/ABXA20150722101.md): Structure · cracked · Jul 22, 2015 · N793AX · Boeing 767281 · Fuselage Miscellaneous Structure
  > LEFT 1809 OUTER CHORD SHOWS A CRACK INDICATION, AT 3 EACH FASTENERS IN AREA 3, ON THE AFT SIDE OF CHORD. REPLACE LT 1809-5 CHORD SECTION, PN 015T1059-3 IAW REA B653-61651-MR. SDR INFO CRACKED 1/8", NO CRACK HOLES WERE ELONGATED. PN 015T1059-3, SN NA, PART NA
- [SDR ABXA20150722097](https://openairdocs.org/sdr/ABXA20150722097.md): Support Rib · corroded · Jul 22, 2015 · N793AX · Boeing 767281 · Wing, Rib/Bulkhead
  > WING REAR SPAR TO TE PANEL ATTACH BEAM FWD OF HINGED ACCESS PANEL 651YBX, SPLIT ON EDGE. REMOVED PANEL 651YBX. R & R PANEL ATTACH BEAM IAW SRM 51-40-02 PARA 7D & REA B657-61642. RE-INSTALLED PANEL 651YBX IAW SRM 51-40-02 PARA 7D. CORRODED LEVEL 2, PN 113T1
- [SDR ABXA20150721100](https://openairdocs.org/sdr/ABXA20150721100.md): Panel Support · corroded · Jul 21, 2015 · N793AX · Boeing 767281 · Wing Miscellaneous Structure
  > LOWER WING TE PANEL ATTACH CHORD AT WS 1054, SPLIT ON EDGE INBD OF AUX TANK VENT. R & R LT WING TE PANEL SUPPORT CHORD WS 1054 IAW SRM 51-40-02 & REA B657-61637. CORRODED L2, PN 113T1676-19, SN NSN, PART NAME PANEL SUPPORT CHORD, STRINGER & WS LOCATION ON AC
- [SDR ABXA20150721099](https://openairdocs.org/sdr/ABXA20150721099.md): Panel Support · corroded · Jul 21, 2015 · N793AX · Boeing 767281 · Wing Miscellaneous Structure
  > LOWER TE PANEL, ATTACH CHORD AT WS 827, CORRODED AROUND NUTPLATE. R & R LT WING TE PANEL SUPPORT CHORD IAW SRM 51-40-02, EA B657-61631. CORRODED L2, PN 113T1672-5, SN NSN, PART NAME PANEL SUPPORT, STRINGER & WS LOCATION ON ACFT WS 827. ACFT WAS GNDED.
- [SDR ABXA20150721094](https://openairdocs.org/sdr/ABXA20150721094.md): Panel Support · corroded · Jul 21, 2015 · N793AX · Boeing 767281 · Wing Miscellaneous Structure
  > REAR SPAR TO WING TE LOWER PANEL ATTACH CHORD SPLIT ON EDGE, AT WS 930. R & R RT WING TE LOWER PANEL ATTACH CHORD AT WS 930 IAW SRM 51-40-02 & REA B657-61634. CORRODED L2, PN 113T1683-28, SN N/A, PART NAME PANEL SUPPORT, STRINGER & WS LOCATION ON ACFT WS 930
- [SDR ABXA20150721093](https://openairdocs.org/sdr/ABXA20150721093.md): Panel Support · corroded · Jul 21, 2015 · N793AX · Boeing 767281 · Wing Miscellaneous Structure
  > REAR SPAR TO TE LOWER PANEL ATTACH CHORD SPLIT ON EDGE, AT WS 944. R & R RT WING TE LOWER PANEL ATTACH CHORD, AT WS 9644 IAW SRM 51-40-02 & REA B657-61636. CORRODED L2, PN 113T1675-22, SN N/A, PART NAME PANEL SUPPORT, STRINGER & WS LOCATION ON ACFT WS 944.
- [SDR ABXA20150721092](https://openairdocs.org/sdr/ABXA20150721092.md): Panel Support · corroded · Jul 21, 2015 · N793AX · Boeing 767281 · Wing Miscellaneous Structure
  > REAR SPAR TO TE LOWER PANEL ATTACH CHORD SPLIT ON EDGE, AT WS 1054, AT AUX TANK VENT. R & R RT WING TE LOWER PANEL ATTACH CHORD WING STATION 1054 IAW 51-40-02 & REA B657-61635. CORRODED L2, PN 113T1676-22, SN NA, PART NAME PANEL SUPPORT, STRINGER & WS LOCATIO
- [SDR ABXA20150720102](https://openairdocs.org/sdr/ABXA20150720102.md): Beam · corroded · Jul 20, 2015 · N793AX · Boeing 767281 · Wing Main, Frame Structure
  > REAR SPAR TO TE PANEL, ATTACH BEAM UPPER CHORD EXFOLIATED AROUND OTBD NUTPLATES AT STATION 288, INBD OF GEAR TRUNNION. REMOVED PANELS FOR ACCESS, REMOVED CORRODED UPPER CHORD. INSTALLED NEW UPPER CHORD, PN 113T1623-125, RE-INSTALLED, REMOVED PANELS, PANELS T
- [SDR ABXA20150717095](https://openairdocs.org/sdr/ABXA20150717095.md): Structure · corroded · Jul 17, 2015 · N793AX · Boeing 767281 · Wing Miscellaneous Structure
  > UPPER CHORD SPLIT ON EDGE & CORRODED AROUND NUTPLATES ON REAR SPAR TO TE BEAM, AT WS 285, 14 INCHES FROM REAR SPAR M, INBD OF GEAR TRUNNION. REMOVED RT WING UPPER TE PANELS. R & R TE UPPER CHORD AT WW 285.14 IAW SRM 51-40-02 PARA 4.6 & 7D. INSTALLED PANEL A
- [SDR ABXA20150715104](https://openairdocs.org/sdr/ABXA20150715104.md): Angle · corroded · Jul 15, 2015 · N793AX · Boeing 767281 · Fuselage Main, Keel
  > LOWER ANGLE AT KEEL TO STATION 999 BULKHEAD CORRODED. REMOVED PANEL 149AL FOR ACCESS. REMOVED LOWER ANGLE, FOUND OUT OF LIMITS. REPLACED LOWER ANGLE IAW DWG 145T8610, INSTALLED LOWER ANGLE IAW SRM 51-40-02. INSTALLED PANEL 149 AL IAW SRM 51-40-02. CORRODE
- [SDR ABXA20150713120](https://openairdocs.org/sdr/ABXA20150713120.md): Stiffener · corroded · Jul 13, 2015 · N793AX · Boeing 767281 · Wing Miscellaneous Structure
  > LEFT WING TE PANEL SUPPORT AT WS 280 HAS A CORRODED T STIFFENER, 31" AFT OF THE WING SKIN TE, PN 113T1623-19. REMOVED CORRODED STIFFENER, FABRICATED NEW FROM & 10136-2001 PO 0020699, TAG 1386185 IAW DWG 113T1623. INSTALLED NEW STIFFENER IAW SRM 51-40-02. SD
- [SDR ABXA20150710091](https://openairdocs.org/sdr/ABXA20150710091.md): Strut · corroded · Jul 10, 2015 · N793AX · Boeing 767281 · Wing Spar
  > NUMBER 2 SLAT OTBD AUX TRACK ATTACH FITTING, LOWER OTDB STRUT CORRODED AROUND NUTPLATE AT FWD END. R & R STRUT IAW DWG 114T2224 & SRM 51-40-02 STEP 7. CORRODED L2, PN 114T2224-15, PART NAME STRUT, STRINGER LOCATION WS 937 4 EDGE. ACFT WAS GNDED.
- [SDR ABXA20150708118](https://openairdocs.org/sdr/ABXA20150708118.md): Support Fitting · corroded · Jul 8, 2015 · N793AX · Boeing 767281 · Wing, Attach Fittings
  > LEFT WING NR 1 FLAP SUPPORT, RIB NR 4 HOLE SHOWS CRACK INDICATION WITH EDDY CURRENT. REAMED HOLE TO FINAL SIZE OF.7495.7505 ON FLAP SUPPORT NR 1, HOLE NR 4 IAW REA B657-61641-MR. SDR INFO CORRODED L2, PN 113T1345-43, SN NONE, PART NAME NR 1 FLAP SUPPORT FI
- [SDR ABXA20150708117](https://openairdocs.org/sdr/ABXA20150708117.md): Support Fitting · corroded · Jul 8, 2015 · N793AX · Boeing 767281 · Wing, Attach Fittings
  > LEFT WING NR 1 FLAP SUPPORT, RIB NR 3 HOLE SHOWS CRACK INDICATION WITH EDDY CURRENT. REAMED HOLE TO FINAL SIZE OF.7495.7505 ON FLAP SUPPORT NR 1, HOLE NR 3 IAW REA B657-61641-MR. SDR INFO CORRODED L2, PN 113T1345-43, SN NONE, PART NAME NR 1 FLAP SUPPORT FI
- [SDR ABXA20150708116](https://openairdocs.org/sdr/ABXA20150708116.md): Support Fitting · corroded · Jul 8, 2015 · N793AX · Boeing 767281 · Wing, Attach Fittings
  > REAMED HOLE TO FINAL SIZE OF 3.7495.7505 ON FLAP SUPPORT NR 1, HOLE NR 2 IAW REA B657-61641-MR. CORRODED L2, PN 113T1345-43, SN NONE, PART NAME NR 1 FLAP SUPPORT FITTING, STRINGER & WS LOCATION ON ACFT WS 797. ACFT WAS GNDED.
- [SDR ABXA20150708115](https://openairdocs.org/sdr/ABXA20150708115.md): Support Fitting · corroded · Jul 8, 2015 · N793AX · Boeing 767281 · Wing, Attach Fittings
  > LEFT WING NR 1 FLAP SUPPORT, RIB NR 1 HOLE SHOWS CRACK INDICATION WITH EDDY CURRENT. REAMED HOLES TO FINAL SIZE OF.7495 &.7505 IAW REA NR B657-61641MR. SDR INFO CORRODED L2, PART NUMBER 113T1345-43, PART NAME NR 11 FLAP SUPPORT FITTING, STRINGER & WS LOCAT
- [SDR ABXA20150708114](https://openairdocs.org/sdr/ABXA20150708114.md): Support Fitting · corroded · Jul 8, 2015 · N793AX · Boeing 767281 · Wing, Attach Fittings
  > RIGHT WING NR 7 FLAP SUPPORT, RIB NR 4 HOLE SHOWS CRACK INDICATION WITH EDDY CURRENT. REAMED HOLE TO FINAL SIZE OF.8745 &.88.55 IAW REA NR B657-61641-MR. CORRODED L2 PN 113T1345-48, PART NAME NR 7 FLAP SUPPORT FITTING, SN NSN, STRINGER LOCATION WB 61G.2.
- [SDR ABXA20150708113](https://openairdocs.org/sdr/ABXA20150708113.md): Support Fitting · corroded · Jul 8, 2015 · N793AX · Boeing 767281 · Wing, Attach Fittings
  > RIGHT WING NR 7 FLAP SUPPORT, RIB 11 HOLE SHOWS CRACK INDICATION WITH EDDY CURRENT. REAMED HOLE TO FINAL SIZE OF.8745 &.8755 IAW REA NR B657-61641-MR. SDR CORRODED L2, PN 113T1345-48, PART NAME NR 2FLAP SUPPORT FITTING, SN NSN, STRINGER LOCATION WB 61G.2.
- [SDR ABXA20150708112](https://openairdocs.org/sdr/ABXA20150708112.md): Support · corroded · Jul 8, 2015 · N793AX · Boeing 767281 · Wing, Attach Fittings
  > RIGHT WING NR 8 FLAP SUPPORT, RIB NR 3 HOLE SHOWS CRACK INDICATION WITH EDDY CURRENT. REAMED HOLE TO FINAL SIZE OF.7495 &.7505 IAW REA NR B767-61641-MR. SDR CORRODED L2, PN 113T1345-44, PART NAME 8 FLAP SUPPORT F1 WING, SN NSN, STRINGER LOCATION WS 807. A
- [SDR ABXA20150708111](https://openairdocs.org/sdr/ABXA20150708111.md): Support Fitting · corroded · Jul 8, 2015 · N793AX · Boeing 767281 · Wing, Attach Fittings
  > RIGHT WING NR 8 FLAP SUPPORT, RIB NR 2 HOLE SHOWS CRACK INDICATION WITH EDDY CURRENT. REAMED HOLE TO FINAL SIZE OF.7493.7505 ON FWD SUPPORT NR 8, HOLE NR 2 IAW REA B767-61641-MR. SDR CORRODED L2, PN 113T1345-44, PART NAME 8 FLAP SUPPORT FITTING, SN NSN, ST
- [SDR ABXA20150706103](https://openairdocs.org/sdr/ABXA20150706103.md): Angle · corroded · Jul 6, 2015 · N793AX · Boeing 767281 · Fuselage Main, Keel
  > LOWER ANGLE AT KEEL TO STATION 977 BULKHEAD LBL 5 CORRODED. R & R LOWER ANGLE KEEL STATION 977 IAW SRM 51-40-02 & DWG 145T8610. CORRODED L2, PN 145T8610-9, SN NSN, PART NAME ANGLE, FS LOCATION ON ACFT, 977 LT WW, KEEL STRINGER & WS LOCATION ON ACFT LBL 5. A
- [SDR ABXA20150624090](https://openairdocs.org/sdr/ABXA20150624090.md): Rib · corroded · Jun 24, 2015 · N793AX · Boeing 767281 · Wing, Rib/Bulkhead
  > NUMBER 5 SLAT OTBD AUX TRACK, INBD LOWER STRUT CORRODED AROUND FWD NUTPLATE. REMOVED DAMAGED STRUT RIB & INSTALLED NEW STRUT RIB PN 114T2203 13AX IAW SRM 51-40-02. CORRODED LEVEL 2, PN 114T2203-15, PART NAME STRUT AIR LOAD RIB, FS & BS LOCATION LW, STRINGER
- [SDR ABXA20131011649](https://openairdocs.org/sdr/ABXA20131011649.md): Bulkhead · cracked · Oct 11, 2013 · N793AX · Boeing 767281 · Fuselage Main, Bulkhead
  > DURING A HFEC INSPECTION OF THE Y RING ATTACHMENT OF THE AFT PRESSURE BULKHEAD A CRACK WAS INDICATED AT A FASTENER HOLE LOCATED AT STRINGER 10R B STATION 1582 INTERIOR OF THE FUSELAGE. TIMED OUT VERIFIED CRACK & REPAIRED IAW REA B653-60742-MR, TRIM OUT MEASUR
- [SDR ABXA20131011646](https://openairdocs.org/sdr/ABXA20131011646.md): Strut · corroded · Oct 11, 2013 · N793AX · Boeing 767281 · Leading Edge Devices
  > NUMBER 5 SLAT INBD AUX TRACK OTBD LOWER STRUT HAS CORROSION UNDER NUTPLATES. R & R NR 5 SLAT INBD AUX TRACK OTBD LOWER RIB STRUT PN 114T2201-23 IAW REA NR B657-60734-MR AND B767 SRN 51-40-02. PN 114T2201-23, NSN, STRUT RIB CORRODED AT 433.1 TO 434.1. AIRCR
- [SDR ABXA20131010648](https://openairdocs.org/sdr/ABXA20131010648.md): Stringer · cracked · Oct 10, 2013 · N793AX · Boeing 767281 · Fuselage Main, Longeron/Stringer
  > FORWARD LOWER CARGO STRINGER 23L AFT OF STATION 767 FRAME HAS A 1.1 INCH CRACK AT STRINGER END FITTING LOC. REPAIRED STRINGER 23L AT STATION 676 TO 700 IAW B767-SRM 53-00-03 FIG 201 REPAIR 2. PN143T3001, NSN, STRINGER CRACKED 1.3 INCHES AT 676, 23L. AIRCRA
- [SDR ABXA20131006645](https://openairdocs.org/sdr/ABXA20131006645.md): Bracket · cracked · Oct 6, 2013 · N793AX · Boeing 767281 · Trailing Edge Flaps
  > BRACKET ON FLAP ANGLE GEARBOX 18 INCHES FROM FUSELAGE ON WING TE CRACKED. R & R ANGLE GEARBOX BRACKET IAW B767-SRM 51-40-02 P. 10 PN 256T3022+-7, NSN, BRACKET CRACKED 1/2 INCH AT WBL 121 TO WBL 124. AIRCRAFT WAS GROUNDED.
- [SDR ABXA20131003647](https://openairdocs.org/sdr/ABXA20131003647.md): Strut · corroded · Oct 3, 2013 · N793AX · Boeing 767281 · Leading Edge Devices
  > NUMBER 2 SLAT INBD AUX TRACK OTBD LOWER STRUT SPLIT AT FWD EDGE. NES STRUT RIB WAS FABRICATED ON REA B657-60736-MR. INSTALLED NEW STRUT RIB PN 114T2221-17 & A NEW TRACK FTG SHIM PACK IAW B767 SRM 51-40-02 PARA 4 & 7. PN 114T2221-17, NSN, STRUT CORRODED AT O
- [SDR ABXA20130308412](https://openairdocs.org/sdr/ABXA20130308412.md): Contact · dirty · Mar 8, 2013 · N793AX · Boeing 767281 · Emergency Lighting
  > EXTERIOR EMERGENCY EXIT LIGHT FAILS TO ILLUMINATE. CLEANED CENTER CONTACT IN LIGHT SOCKET ASSEMBLY OPS CHECK GOOD IAW B767 AMM 33-51-00, ACFT WAS GROUNDED.
- [SDR ABXA20120907272](https://openairdocs.org/sdr/ABXA20120907272.md): Door · missing · Sep 7, 2012 · N793AX · Boeing 767281 · Landing Gear Doors
  > UPON MX POST FLIGHT WALK AROUND FOUND RIGHT MAIN GEAR SHOCK STRUT DOOR MISSING AND DAMAGE TO RIGHT TRUNNION DOOR. REMOVED AND REPLACED MLG TRUNNION DOOR ASSY W AMM 32-12-11-4, REMOVED AND REPLACED RIGHT MLG SHOCK STRUT DOOR ASSY IAW 32-12-06 AND 32-12-05 JACK
- [SDR ABXA20120717224](https://openairdocs.org/sdr/ABXA20120717224.md): Battery · discharged · Jul 17, 2012 · N793AX · Boeing 767281 · Emergency Lighting
  > ON SERVICE CHECK FOUND EMERGENCY LIGHTS INOP FOR CREW SERVICE AREA. REMOVED AND REPLACED IAW AMM 33-51-07-2, INSTALLED SPARE EMERGENCY LIGHT BATTERY OPS CHECK NORMAL, ACFT WAS GROUNDED.
- [SDR ABXA20120504343](https://openairdocs.org/sdr/ABXA20120504343.md): Fastener · corroded · May 4, 2012 · N793AX · Boeing 767281 · Cargo/Baggage Doors
  > MDCD AFT MID LATCH CAM HOOK PITTED (.005). REPAIRED MDCD AFT MID LATCH CAM PER REA NO: B652-59813-MR AND 767MM 52-32-09-S, ACFT WAS GROUNDED.
- [SDR ABXA20120504342](https://openairdocs.org/sdr/ABXA20120504342.md): Fastener · corroded · May 4, 2012 · N793AX · Boeing 767281 · Cargo/Baggage Doors
  > MDCD FWD MID LATCH CAM HOOK PITTED (.0075). REPAIRED MDCD FWD MID LATCH CMA PER REA NO: B652-59812-MR AND 767 MM 52-32-09-2, ACFT WAS GROUNDED.

Next page: https://openairdocs.org/aircraft/N793AX/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N793AX' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N793AX/reports

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